HIGH SPEED THERMOMECHANICAL ACTUATOR

Abstract: A heat sink (14) provides thermal communication between an actuator (18) and fluid controlled by a valve (12) which is flowing through a conduit (10). The actuator includes a vessel which is defined on its largest surfaces by plates (22, 50) of beryllium oxide thermally conductive ceramic covered with thermally conductive, relatively electrically non-conductive nichrome foil (24, 26). Longitudinal sides (30, 32) of the vessel are also relatively non-conductive. A thermally and electrically conductive core, such as accordion pleated beryllium copper foil (44) or a carbon fiber mat (82, 116) is disposed in the chamber. Electrical current flows through the core itself (Figure 4) or through electrically insulated heating wires (80) (Figure 5) or through an electrically insulated heating surface layer (Figure 6) causing resistance heating and melting of a non-gaseous polymeric phase change compound (46). The resistance heating current is inductively induced in the embodiment of (Figure 8). The polymeric core material expands transferring force through a rubber core (66, 108) to a push pin (68, 130). Fluid flowing through the conduit (10) draws heat from the phase change material through the core, the vessel, and the heat sink to solidify the phase change compound, causing the push pin to be retracted. The phase change compound is selected and the actuator is sized to achieve an actuation time of less than 500 milliseconds.

Description: HIGH SPEED THERMOMECHANICAL ACTUATOR Technical Field The present invention relates to mechanical power supplies and actuators. It finds particular application in conjunction with high force, low travel extensible actuators and will be described with particular reference thereto. However, it is to be appreciated that the invention will also find application in conjunction with other high pressure fluid systems, as well as other mechanical power supplies, pumps, motors, valve controllers, and the like. Background Art Heretofore, numerous techniques have been utilized for converting thermal expansion into mechanical power. The large power levels generated by thermal expansion have been converted to useful work in heat engines and other devices. Most commonly, the energy of a liquid/vapor phase thermal expansion is harnessed to capitalize on the ready transportability of liquids. The transportability facilitates a mass transfer of heat for effecting phase change. One way to effect the mass transfer is by physically moving the liquid to a heat source, then allowing the liquid/vapor to flow against resistance to a cooling source. Steam and other types of external combustion engines typify this technique. In another technique, fuel liquids or liquid aerosols are pumped into a combustion chamber. The mix is ignited and the combustion vapor is permitted to exit the chamber against resistance, physically removing the heat and clearing the chamber for the next cycle. These liquid/vapor phase techniques have several drawbacks. First, the vapor phase is compressed at very high pressures. An unanticipated release of these pressures creates shock waves associated with a blast, hurling debris in a dangerous manner. The material is transported and expended, requiring complex controls and valving, as well as a continuous supply of liquid to replace the liquid lost or consumed. Rather than transporting the material which is acted upon by the heat to expand and contract, the heat itself may be moved. More specifically, heat can be conducted into and out of a sealed chamber which expands during the heating cycle and contracts during the cooling cycle. The sealed chamber technique has many advantages including its mechanical simplicity, proportional control, high stiffness actuation, ready adaption to a variety of heat sources, high power density, and silent operation. Moreover, because liquids compress only a small amount, as compared to vapors, they tend to be much safer than a liquid/vapor system. Unfortunately, the transfer of heat into and out of the medium normally relies on thermal conductivity. Mediums which exhibit good expansion/ contraction ratios upon melting have relatively poor thermal conductivities. Thus, a solid/liquid sealed chamber phase change actuator tends to have a very slow cycle time. The present invention contemplates a new and improved solid/liquid or solid/solid phase change sealed chamber actuator which can exhibit a reduced cycle time on the order of the cycle time of a solenoid, i.e. about one half second or less. Summary of the Invention An actuator includes a vessel which defines an interior chamber, a thermally conductive core disposed within the chamber, a temperature expansive component fills paths within the core. In this manner, as the core conducts heat into the compound, it expands; and as the core conducts heat out of the compound, it contracts , . A mechanical movement means undergoes mechanical movement as the compound expands and contracts. The actuator is further characterized by a means for selectively creating a temperature differential ΔT between a heat sink and the core for moving heat out of the phase change compound such that UAΔT f < n o.5 -.s a£ e ir cm. Hf where, U is a heat transfer coefficient of the compound, ΔT is the temperature differential, A is the representative area of a conductive path from the core into the compound, and H f a heat of fusion of the compound. The actuator is further characterized by the core including carbon fiber, which has a high thermal conductivity. The actuator is further characterized by a means for selectively compressing the carbon fibers of the core to adjust their thermal conductivity. In accordance with another aspect of the present invention, the core includes a conductive accordion pleated foil. In accordance with another aspect of the present invention, the interior chamber is generally annular and surrounds a magnetic flux conductive core. A primary winding selectively induces magnetic flux in the core. A secondary winding induces magnetic flux in the core such that an electric current is induced in the secondary winding without electrical feeds through the vessel. In accordance with another aspect of the present invention, an actuator includes a vessel which defines an interior chamber, a compound which expands and contracts as it is heated and cooled disposed in the chamber, and a means for converting expansion and contraction of the compound into mechanical movement. The actuator is further characterized by a carbon fiber core disposed within the chamber and defining a multiplicity of paths between surfaces of the carbon fiber. The carbon fiber is in thermal communication with a thermally conductive portion of the vessel. The compound fills the paths within the carbon fiber such that the carbon fiber conducts heat into the compound to cause it to expand and conducts heat out of the compound causing it to contract. In accordance with another aspect of the present invention, a method of mechanical actuation is provided. An interior chamber of a vessel which holds a thermally conductive core defining a multiplicity of paths between surfaces thereof is filled with a compound which expands and contracts as it is heated and cooled. Heat is added to the core causing the compound to expand and the expansion is converted into mechanical motion. Heat is removed from a heat sink in thermal communication with the core, cooling the compound and causing it to contract. The contraction is converted into mechanical contraction. The core is thermally connected with the heat sink such that the mechanical contraction occurs in less than 0.5 seconds. More specifically, UAΔT/H f < 0.5 seconds, where U is a heat transfer coefficient of the compound, T is a temperature differential, A is a representative area of a conduction path from the core into the compound, and H f is a heat of fusion of the compound. In accordance with a more limited aspect of the present invention, the method includes selectively compressing carbon fibers of the core for adjusting a volume to surface ratio. In accordance with another more limited aspect of the present invention, a heating current in the internal chamber of the vessel is inductively induced. One advantage of the present invention resides in its speed of operation. The present design permits speeds which are comparable with a solenoid. Another advantage of the present invention resides in its mechanical simplicity. Another advantage of the actuators in accordance with the present invention resides in their high stiffness. Other advantages include proportional control, high power densities, silent operation, safety, and flexibility of heat sources. Brief Description of the Drawings FIGURE 1 is a diagrammatic illustration of an actuator in accordance with the present invention in combination with a fluid valve; FIGURE 2 is a longitudinal sectional view of the actuator of FIGURE 1; FIGURE 3 is a transverse sectional view of the actuator of FIGURE 1; FIGURE 4 is an exploded view of the actuator of FIGURE 1; FIGURE 5 is an exploded view of an alternate embodiment in which the core includes a fibrous mat; FIGURE 6 is an alternate embodiment in which the core includes a spiral wrapped fabric of high thermal conductivity fiber; FIGURE 6A is an enlargement of a portion of FIGURE 6; FIGURE 7 plots thermal conductivity of the core of FIGURE 6 versus the rest compressive force within the core; and, FIGURE 8 is an inductively controlled alternate embodiment. Detailed Description of the Preferred Embodiments With reference to FIGURE 1, a conduit 10 carries fluid, e.g. hydraulic fluid, to a control valve 12. Preferably, the fluid has a temperature below about 150° F. Typically, hydraulic systems include a heat exchanger to keep hydraulic fluids cooled to temperatures below 140° F. Numerous other fluid systems convey fluid vthich consistently has a temperature in this range, e.g. "cold" water systems, radiant heating systems, lower temperature chemical processing systems, and the like. A first interface or heat sink member 14 provides thermal communication with the conveyed fluid. Preferably, the first heat sink or interface means includes a cylinder of aluminum, copper, or other highly thermal conductive material through which the fluid passes, e.g. part of the valve body. With continuing reference to FIGURE 1 and particular reference to FIGURES 2, 3, and 4, the actuator 18 includes a second or actuator heat sink 20 which is mounted against the mounting surface 16 of the first heat sink member 14. A layer of a high thermal conductivity material 22 is connected in thermal communication with the second heat sink 20. Preferably, the high thermal conductivity layer 22 has a relatively low electrical conductivity to inhibit electrical current from flowing therethrough to the second heat sink 20. In the preferred embodiment, the layer 22 is a beryllium oxide ceramic. Opposite layers of a metallic film or foil 24, 26, and edge members 30, 32, 34, 36 form a vessel which defines a chamber therein. The metallic film or foil layers 24, 26 and the side members 30, 32 are again constructed of a thermally conductive material with a relatively low electrical conductivity. Opposite end members 34, 36 are constructed of a material with good electrical conductivity, e.g. copper or beryllium copper. Electrical connection terminals 40, 42 are connected with the end members 34, 36, respectively. A core member 44 is fabricated from 0.10 mm beryllium copper foil which is folded into a pleated section, e.g. by rolling between gear-like rollers. The foil is collapsed until the selected spacing, e.g. 0.05 mm, exists between adjacent walls of the core. The pleated core is brazed to the nichrome foils 24, 26, the nichrome side members 30, 32, and the copper or electrically conductive ends members 34, 36. The passages in the pleated foil are filled with a thermal expansion material 46, such as wax, which expands as it undergoes a solid-solid phase change at its glass transition temperature, a solid-liquid phase change at its melting temperature, or the like. With thin passages 0.05 mm apart, all portions of the phase change material are less than 0.025 mm from the core member. This dimension may be decreased for a higher speed actuator or increased where lower speeds are acceptable. When an electrical current is applied between electrical connectors 40, 42, a voltage or current divider is effectively defined in which most of the current is channeled through the core foil 44. That is, a nichrome leg including nichrome foil 22, 26 and nichrome side members 30, 32 has a relatively high electrical resistance. A core leg including the core 44 and the end members 34, 36 has significantly less electrical resistance. With these two legs effectively connected in parallel, the current flows primarily through lower resistance leg in accordance with the relative resistance of the two legs. An adjustable current source 48 provides a large burst or pulse of current to cause initial actuation and applies lower amounts of current to cause sufficient heating to offset cooling through the heat sinks to hold a preselected state of actuation of extension. A second layer of the beryllium oxide or other thermally conductive material 50 is applied to an opposite face of the vessel. A reinforcing layer 52 overlays the second face to strengthen the chamber against buckling or expansion. A mechanical movement transfer means 60 converts expansion of the expansion medium 46 into mechanical movement. In the preferred embodiment, the means 60 includes a cylindrical fitting 62 which is held firmly against one of the layers of nichrome foil 24, 26. The nichrome foil has a portion 64 which is purposely not brazed to the core 44 to enable it to flex outward from the chamber as the expansion material changes phase, i.e. to function as a snap dome member. A deformable, resilient member 66, e.g. a rubber plug or core, is disposed in the cylindrical fitting 62 for transferring mechanical movement from the dome member 64 to a push pin 68. A threaded plug 70 is torqued down to compress the rubber core to preload the push pin 68. By selectively adjusting the torque on the rubber member, the starting dimension or extensional point of the push pin is calibrated. The rubber core 66 also functions analogous to a hydraulic fluid to transform the low travel, high area deflection of the dome member 64 into a higher travel, smaller cross-sectional area deflection of the push pin 68. With reference to FIGURE 5, in another embodiment, the core 44 is a high thermal conductivity carbon fiber, preferably K-1100 carbon fiber, available from Amoco, which has a thermal conductivity about five times as high as beryllium copper. More specifically, the thermal conductivity of K-1100 carbon fiber is on the order of 640 btu/ft-°F-Hr. Carbon fiber or beryllium copper foil cores have relatively low electrical resistance, necessitating high amperage, low voltage power supplies. If low amperage, high voltage supplies are desired, a heater such as a resistance wire 80 can be included in the core. This wire is insulated from the core heat transfer materials. Alternately, a thin film of metal can be plated onto an insulating layer on either internal core surface and be in contact with the carbon fiber or beryllium copper core structures. This thin film, either applied by flame spray, sputtering, electrophoresis, or other means, is also electrically insulated at its contact with the core heat transfer structure. The carbon fibers readily conduct heat from the resistance wire to all regions of the thermally expansive material. Because the carbon fibers are highly electrically conductive, the resistance heating wire 80 is electrically insulated. Thermally conductive electrical insulators 82, such as beryllium oxide, prevent the carbon fiber from electrically shorting the terminals 40, 42. Ends of the electrical resistance wire are electrically interconnected with the high pressure electrical feedthroughs 40 and 42 to provide for selective heating in the vessel. The fiber core may be a random fiber mat or felt which is impregnated with the thermally expansive medium, such as a thermally expansive polymer. Alternately, the carbon fibers may be woven into a cloth, fashioned into rovings, wound on a mandrel or put into other shapes or configurations. Further, the fibers may be randomly chopped. To facilitate manufacture, a soup of the melted thermally conductive material and finely divided carbon fibers may be mixed and loaded into the vessel. Further, other highly thermally conductive materials may also be introduced into the mix, such as diamonds. Industrial diamonds have a thermal conductivity which is about a third again more than the K-1100 carbon fiber. By intermixing an industrial diamond dust into the mixture, still better thermal conductivity can be provided. Alternately, the core can be comprised of finely divided diamonds. FIGURE 6 shows a preferred mandrel wound or coaxial carbon fiber, carbon filament embodiment. The vessel is defined by a highly thermally conductive metal member 100 which defines a generally annular bore therein. The bore has a tapered inner end 102 in which a tapered beryllium copper collet 104 is slidably received. An annular chamber 106 is defined between the collet and a rigid non-compressible metal element 110. The collet 104 has a lip 112 which restrains the metal element 110 from shifting rearward. An 0-ring 114 inhibits high pressure leakage of the thermally conductive material and prevents air from being drawn into the annular region 106 as the thermally expansive material contracts. The annular chamber 106 is filled with tightly, mandrel wound carbon fibers 116 impregnated with the thermal expansion material. The fibers 116 are depicted as widely spaced in FIGURE 6A for simplicity of illustration. A thin electrical resistive heater layer 118 extends substantially around the annular chamber and are surrounded by thermally conductive electrical insulation 120. Optionally, electrically insulated resistance wires may be disposed in the annular chamber 106. High pressure electrical feeds 122 provide insulated electrical current flow paths between the resistance heater layer 118 and the exterior of the actuator. A fill tube 124 is provided to facilitate filling of the annular bore 106 with the. thermally expansive material. A force transfer means transfers expansive force from the annular region 106. In the preferred embodiment, a plurality of radial bores 126 are filled with the polymeric expansion material 128. Under the high forces generated in the annular region 106, the polymeric expansion material flows to transfer the force even in its cool state. The radial bores 126 merge such that the polymeric expansion material 128 acts against a piston 130 which is slidably received in a piston guide 132. An O- ring 134 and collar 136 are selectively clamped against the piston by threading the piston guide 132 into or out of the housing 100. In this manner, as the thermally expansive material changes phase and expands, it moves through the bores urging the piston to extend. The collet 104 is threadedly connected 138 with the vessel 100. In this manner, rotation of the collet member 104 by engaging bores 140 forces the collet member 104 against the tapered wall surface 102. The camming contracts the diameter of the collet and compresses the carbon fiber and thermal expansion material within the annular chamber 106. With reference to FIGURE 7, compressing the carbon fibers increases their electrical conductivity, hence their thermal conductivity. The improvement in thermal conductivity might be attributable to pressing crossing fibers together into better thermal contact. The collet includes collet flex points 142 and an O-ring 144 and hydraulic backup ring 146 to facilitate adjusting the compressive force with which the collet is forced into the bore. By selectively adjusting the threaded interaction of the collet and the housing, the conductivity of the carbon fiber is adjusted within the range of available conductivities of FIGURE 7. In the embodiment of FIGURE 8, the actuator is inductively controlled. Electrically conductive carbon fibers 150 are wound tightly around a ceramic or iron magnetic flux conductive core 152 in a recessed region 154. The recessed region is connected by radial bores 156 to a central bore 158. A piston 160 with sealing O-rings 162 is slidably received in the central bore. A thermally conductive outer wall 164 closes the recess to define a closed annular chamber. The outer wall is preferably constructed of beryllium oxide ceramic to avoid parasitic induction of the magnetic field by the outer housing. O- rings 166 seal the annular chamber. The annular chamber including all voids among the tightly wound carbon filaments and the radial and central bores are filled with a polymeric expansion medium 168, such as wax. As the expansion medium in the annular chamber changes state and expands, the polymeric material in the radial and central bores is put under sufficient pressure that it flows, even without changing state. As the polymeric material flows, it forces the piston to extend. Alternately, bores 156, 158 can be filled with an elastomeric compound capable of transferring the expansion to the piston. In this embodiment, the expansion polymer is restricted to area 150. The iron or ceramic magnetic core extends in a loop. A wire winding 170 is wrapped around a remote portion of the core loop for selectively generating magnetic flux through the loop and the electrical carbon fiber winding 150. The speed of the actuator is, in large part, controlled by the speed with which thermal energy is moved into and out of the expansion medium. Because solenoids are among the most common actuators, a high proportion of existing equipment is designed to use actuators which operate at solenoid speeds. Analogously, many designers require actuators to have speeds comparable to solenoids. Under load, solenoids typically operate in a range of about 50-500 milliseconds. Without load, solenoids might act as fast as 20 milliseconds. Accordingly, the core construction of the present actuator is designed to move heat into and out the expansion medium at a sufficient rate that actuation can be achieved in a. half second or less. The amount of heat energy Q c required to expand the actuator is determined by the heat of fusion H f of the expansion medium, the pressure P generated, and the expansion volume dV. The amount of heat energy Q c which must be removed to contract an expanded actuator is solely the heat of fusion H f . The heat of fusion is a complex function of pressure and temperature which varies for different polymeric materials which is not readily reducible to a universal mathematical formula. For simplicity in the present analysis, the heat of fusion is represented as a fixed quantity H f . More specifically: Expanding: Q c = H f + P*dV*c (la) Contracting: Q c = H f (lb) , where c is a conversion factor. When Q is measured in BTU per cubic inch, the heat of fusion H f is measured in BTU per cubic inch, the pressure P in pounds per square inch, and the expansion volume dV in cubic inches per cubic inch of expansion material volume, the conversion factor C is 1/9336 BTU per inch/pound. The heat transfer rate, q, is the time derivative of the heat energy Q, i.e. Expanding: q c = dQ c /dt = d(H f + P*dV*c)/dt (2a) Contracting: q c = dQ_/dt = dH f /dt (2b) . In the cooling or contracting mode, the rate is controlled by the overall heat transfer coefficient U which describes the net thermal conductance of a total path between the heat sink and the expansion material. This path extends from the heat sink to furthest most incremental element of the expansion material which undergoes the phase change. It will be noted, that all phase change material need not undergo the phase change to affect contraction of the actuator. However, material which has not undergone the phase change does not contribute the actuation. Heat transfer rate q c is also defined by: q c = UAΔT (3), where U is the overall heat transfer coefficient, A is the representative area of the conduction path, and ΔT is the overall temperature difference between the expansion material and the heat sink. Combining Equations (2) and (3): Contracting: UA = q c /ΔT = (dH f /dt) /ΔT (4a) . In the above calculations, U, the overall heat transfer rate is a conglomerate number which represents the thermal conductivity factors of the various materials in the path, such as the nichrome foil, the beryllium oxide ceramic, the expanding polymer and the various sinks. In addition, it assumes a conglomerate geometry which can be represented by a theoretical area A, and a length factor, X, which is included in U. In order to amplify the geometry factor, we note that the thermal resistances of the various sink path materials are much lower than that of the expandable polymer. Typical thermal conductivities for sink materials are 240 to 1280 times more thermally conductive than the polymer. Hence, we can approximate the problem by examining the polymer conductivity and geometry alone. In this case, the overall heat transfer coefficient, U, is replaced by the polymer heat transfer coefficient, K- . The expandable polymer element which is farthest from the sink is defined as a distance x through polymer away from the nearest core sink path element. Hence, we can rewrite Equation (3) as: q c = (KA/x)ΔT (5), where A is now an exact area of the conduction path which services the unitary volume of expanding polymer element under consideration. Knowing that K is a constant for the polymeric material, and fixing ΔT to a constant for this analysis, we have: q. = c*A/x (6) , where C=K*ΔT. We can now see that the speed of an actuator is increased by spreading a given volume of polymer in thinner layers (reducing x) over more sink surface area (increasing A) . Our purpose is to define a universal actuator speed factor, and independent of the volume or physical size of any given actuator, hence we must normalize the q c in the Equation 6 above by dividing by the volume of the actuator, as follows: q c /V = (c*A/x)/V = c/x 2 (7) . Since this is a factor for relative comparison of different systems, for convenience we can set c=l and use the square root of the 1/x 2 factor since it is maximized at the same points. We note that this factor is also equal to the internal surface area divided by the internal volume, which is convenient for many comparisons. Hence, our factor becomes: R = A/V = 1/x (8), or for a given volume of actuator, the speed is proportional to the reciprocal of the average distance from an interior wall. Taking a simple example of a narrow groove or saw cut that is x wide, y deep, and z long, the surface area is 2(x+y)z and the volume is xyz. The surface area to volume ratio, R, can be expressed: R = 2 ( x÷y ) z = 2 ( ± +± ) (9). xyz x y From experimental procedures, it has been found that saw cuts of 0.025 cm wide by 0.150 cm deep produce acceptable results. With this example R=571.4 cm 1 . For fiber cores which have a diameter on the order of 10x10^ * cm, the surface to volume ratio is in the range of 35,000 to 127,500 cm "1 , depending on the density to which the fiber core is compressed. Accordingly, cores with a surface area to volume ratio over about 2500 cm "1 produce acceptable results at a lower speed with a ratio of 37,500 cm '1 producing higher speed actuation.

Claims: CLAIMS: 1. An actuator including a vessel which defines an interior chamber therein; a thermally conductive core disposed within the chamber defining a multiplicity of paths between surfaces thereof; a temperature expansive compound filling the paths within the core such that as the core conducts heat into the compound, it expands and as the core conducts heat out of the compound, it contracts; and a means which undergoes mechanical movement as the compound expands and contracts, further characterized by: a means for selectively creating temperature differentials ΔT between a heat sink and the core, the compound having a heat transfer coefficient U, a conduction path from the core into the compound having a representative area A, and the compound having a heat of fusion H f such that UAΔT < O.ssec. H« 2. The actuator as set forth in claim 1 further characterized by a ratio of an area of the surfaces of the thermally conductive core to a volume of the interior chamber of the vessel is greater than 2500 centimeters" 1 . 3. The actuator as set forth in claim 1 further characterized by the core including an electrically and thermally conductive accordion pleated foil. 4. The actuator as set forth in claim 1 further characterized by electrical connection means electrically connected with opposite ends of the core, the core being relatively conductive and the vessel being relatively non- electrically conductive between the opposite ends of the core such that electrical current applied to the electrical connection means flows primarily through the core, such that the core functions as a resistance heater. 5. The actuator as set forth in claim 1 further characterized by at least one side wall of the vessel including a layer of a thermally conductive ceramic. 6. The actuator as set forth in claim 1 further characterized by the thermally conductive core including at least one of a high thermal conductivity fiber and a high thermal conductivity granular material. 7. The actuator as set forth in claim 6 further characterized by the high thermally conductive granular material including finely divided diamond. 8. The actuator as set forth in claim 6 further characterized by the high thermal conductivity fiber including a carbon fiber. 9. The actuator as set forth in claim 8 further characterized by the core containing an electrically insulated heating conductor. 10. The actuator as set forth in claim 8 further characterized by the carbon fiber being one of a random fiber mat, cloth, rovings, mandrel winding, randomly chopped, and finely divided. 11. The actuator as set forth in claim 8 further characterized by a means for selectively compressing the carbon fibers of the core. 12. The actuator as set forth in claim 8 further characterized by. the core being in thermal communication with at least a thermally conductive portion of the vessel, the thermally conductive portion of the vessel having a thermal conductivity which is less than the thermal conductivity of the thermally conductive core material, such that the lower conductivity of the vessel assists in maintaining the core in thermal equilibrium throughout the chamber. 13. The actuator as set forth in claim 1 further characterized by the interior chamber being generally annular and surrounding a magnetic flux conductive core and further including: a primary winding for selectively inducing magnetic flux in the magnetic flux conductive core; a secondary winding disposed in the interior chamber such that the magnetic flux induced in the magnetic flux conductive core induces a current in the secondary winding, the electric current in the secondary winding causing resistance heating. 14. An actuator including a vessel which defines an interior chamber therein, a compound which expands and contracts as it is heated and cooled disposed in the interior chamber, and a means for converting expansion and contraction of the compound into mechanical movement, further characterized by: a carbon fiber core disposed within the chamber and defining a multiplicity of paths between surfaces of the carbon fiber, the carbon fiber being in thermal communication with a thermally conductive portion of the vessel, the compound filling the paths within the carbon fiber such that as the carbon fiber conducts heat into the compound, the compound expands and as the carbon fiber conducts heat out of the compound, the compound contracts. 15. The actuator as set forth in claim 14 further characterized by electrically insulated resistance heating conductors extending through the fibers in thermal communication therewith. 16. The actuator as ' set forth in claim 14 further characterized by a means for selectively compressing the carbon fiber core to adjust heat transfer characteristics. 17. The actuator as set forth in claim 14 further characterized by: a magnetic flux conductive member extending coaxial to the interior chamber, the carbon fiber core being disposed such that flux in the magnetic flux conductive member induces a resistance heating electric current in the carbon fiber; a primary winding means for selectively inducing the magnetic flux in the magnetic flux conductive member. 18. Amethod of mechanical actuation comprising: filling an internal chamber of a vessel with a thermally conductive core that defines a multiplicity of paths between surfaces thereof which paths are filled with a compound which expands and contracts as it heated and cooled, there being a volume to surface ratio between a volume of the internal chamber and a surface area of the core; adding heat to the core causing the compound to expand; converting the expansion of the compound to mechanical extension; cooling a heat sink in thermal communication with the core to cause the compound to contract; converting the contraction into mechanical retraction; thermal communication between the compound and the core being characterized by UAΔT < 0.5sec. H f where, U is a heat transfer coefficient of the compound, ΔT is the temperature differential, A is a representative area of a conduction path from the core into the compound and H f a heat of fusion of the compound, such that the mechanical retraction is achieved in less than 0.5 seconds. 19. The method as set forth in claim 18 wherein the core includes carbon fibers which are selectively compressed to adjust the volume to surface ratio. 20. The method as set forth in claim 18 wherein the step of adding heat includes: inductively inducing a heating current in the internal chamber.

Inventors: SCHNEIDER EDWARD T, SCHNEIDER, EDWARD, T.
Applicants: SCHNEIDER EDWARD T, SCHNEIDER, EDWARD, T.
Application year: 1994
Main classification: G05D15
IPC codes: F03G7, F16K31, G05D3